| Item type |
紀要論文 / Departmental Bulletin Paper(1) |
| 公開日 |
2015-03-26 |
| タイトル |
|
|
タイトル |
<論文>減速機構試験装置によるパラシュートの研究 |
| 言語 |
|
|
言語 |
jpn |
| 資源タイプ |
|
|
資源タイプ識別子 |
http://purl.org/coar/resource_type/c_6501 |
|
資源タイプ |
departmental bulletin paper |
| その他のタイトル（英） |
|
|
その他のタイトル |
Some Experimental Study on Parachute Dynamics by Utilizing a Deceleration System Simulator |
| 著者 |
雛田, 元紀
松尾, 弘毅
塚本, 茂樹
川口, 淳一郎
HINADA, Motoki
MATSUO, Hiroki
TSUKAMOTO, Shigeki
KAWAGUCHI, Jun'ichiro
|
| 著者所属 |
|
|
|
東京大学宇宙航空研究所 |
| 著者所属 |
|
|
|
東京大学宇宙航空研究所 |
| 著者所属 |
|
|
|
東京大学宇宙航空研究所 |
| 著者所属 |
|
|
|
東京大学宇宙航空研究所 |
| 著者所属（英） |
|
|
|
en |
|
|
Institute of Space and Aeronautical Science, University of Tokyo |
| 著者所属（英） |
|
|
|
en |
|
|
Institute of Space and Aeronautical Science, University of Tokyo |
| 著者所属（英） |
|
|
|
en |
|
|
Institute of Space and Aeronautical Science, University of Tokyo |
| 著者所属（英） |
|
|
|
en |
|
|
Institute of Space and Aeronautical Science, University of Tokyo |
| 出版者 |
|
|
出版者 |
東京大学宇宙航空研究所 |
| 書誌情報 |
東京大学宇宙航空研究所報告
巻 17,
号 1_B,
p. 223-239,
発行日 1981-03
|
| 抄録（英） |
|
|
内容記述タイプ |
Other |
|
内容記述 |
A deceleration system simulator has been developed in order to investigate aerodynamic characteristics of parachute in air-stream of the 2 mφ low speed wind tunnel of Institute of Space and Aeronautical Science, University of Tokyo, and also to simulate a controlled parachute system there in which the model parachute is controlled by extending and/or retracting 8 suspension lines independently, according to respective control signals. The performance of the simulator has been examined preliminarily in the low speed wind tunnel by using small model parachutes of 30-60 cm in deployed cross-sectional diameter, and it has been found that the simulator functionates satisfactorily. Some experiments of parachute deployment have been conducted and the results of opening load behavior have been compared with the numerical result obtained from the analysis. It has been shown that both results are in good agreement with each other. Brief qualitative discussion has been made on the feasibility of practical application of the controlled parachute system to a recovery system of rocket pay-load. |
| ISSN |
|
|
収録物識別子タイプ |
ISSN |
|
収録物識別子 |
0563-8100 |
| 書誌レコードID |
|
|
収録物識別子タイプ |
NCID |
|
収録物識別子 |
AN00161914 |
| 資料番号 |
|
|
内容記述タイプ |
Other |
|
内容記述 |
資料番号: SA0125966000 |
SA0125966.pdf (995.5 kB)
